US9625094B2 - Operating method for a cryo-compressed tank - Google Patents
Operating method for a cryo-compressed tank Download PDFInfo
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- US9625094B2 US9625094B2 US12/792,331 US79233110A US9625094B2 US 9625094 B2 US9625094 B2 US 9625094B2 US 79233110 A US79233110 A US 79233110A US 9625094 B2 US9625094 B2 US 9625094B2
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C7/00—Methods or apparatus for discharging liquefied, solidified, or compressed gases from pressure vessels, not covered by another subclass
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0104—Shape cylindrical
- F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/01—Shape
- F17C2201/0147—Shape complex
- F17C2201/0166—Shape complex divided in several chambers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/03—Orientation
- F17C2201/035—Orientation with substantially horizontal main axis
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2201/00—Vessel construction, in particular geometry, arrangement or size
- F17C2201/05—Size
- F17C2201/056—Small (<1 m3)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0391—Thermal insulations by vacuum
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/0602—Wall structures; Special features thereof
- F17C2203/0612—Wall structures
- F17C2203/0626—Multiple walls
- F17C2203/0629—Two walls
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/01—Mounting arrangements
- F17C2205/0123—Mounting arrangements characterised by number of vessels
- F17C2205/013—Two or more vessels
- F17C2205/0149—Vessel mounted inside another one
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
- F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
- F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
- F17C2205/0323—Valves
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/012—Hydrogen
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/035—High pressure (>10 bar)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
- F17C2223/036—Very high pressure (>80 bar)
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0367—Localisation of heat exchange
- F17C2227/0369—Localisation of heat exchange in or on a vessel
- F17C2227/0376—Localisation of heat exchange in or on a vessel in wall contact
- F17C2227/0379—Localisation of heat exchange in or on a vessel in wall contact inside the vessel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0367—Localisation of heat exchange
- F17C2227/0369—Localisation of heat exchange in or on a vessel
- F17C2227/0376—Localisation of heat exchange in or on a vessel in wall contact
- F17C2227/0383—Localisation of heat exchange in or on a vessel in wall contact outside the vessel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/011—Improving strength
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/03—Dealing with losses
- F17C2260/031—Dealing with losses due to heat transfer
- F17C2260/033—Dealing with losses due to heat transfer by enhancing insulation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/01—Applications for fluid transport or storage
- F17C2270/0165—Applications for fluid transport or storage on the road
- F17C2270/0184—Fuel cells
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/32—Hydrogen storage
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- Y02E60/321—
Definitions
- the invention relates to an operating method for a cryo-compressed tank, in which may be stored the cryogenic hydrogen for supplying a consumer, in particular an internal combustion engine and/or a fuel cell of a motor vehicle under supercritical pressure at 13 bar or more.
- a cryo-compressed tank in which may be stored the cryogenic hydrogen for supplying a consumer, in particular an internal combustion engine and/or a fuel cell of a motor vehicle under supercritical pressure at 13 bar or more.
- the removed hydrogen that has been heated in a heat exchanger is conveyed to a heat exchanger, provided in the cryo-compressed tank, by way of a tank pressure regulating valve and a branch line, which branches off of a supply line leading to the consumer, and, after flowing through the heat exchanger, is introduced into the supply line downstream of the branching off of the branch line.
- cryogenic hydrogen for supplying the vehicle drive unit, configured as an internal combustion engine
- a “sub-critical” storage vessel as the cryo tank
- the typical operating pressure of this storage vessel ranges from 1 bar absolute to 10 bar absolute
- the operating temperatures in the so-called “standard cryogenic operation” range from 20 K (Kelvin) to approximately 30 K. That is, the cryogenic hydrogen, contained in the storage vessel and/or in the inner tank of the same, exhibits these physical values, which lie in the so-called sub-critical range in the pressure-density diagram of the hydrogen.
- cryo-compressed storage system represents an additional known prior art, for which reason reference is made to the aforementioned U.S. Pat. No. 6,708,502 B1, which describes different types of insulated compressed storage systems for cryogenic storage mediums with inner and outer diffusion barriers, which envelop an inner tank made of carbon fiber reinforced plastic.
- the described so-called cryo-compressed storage system can be filled with warm pressurized gas at 350 bar and at low storage capacity or as an alternative with liquid hydrogen at low pressure of approximately 1 bar (absolute) at higher storage capacity.
- cryo-compressed tank which can be designed like the cryo-compressed storage system described in the previous paragraph, supercooled cryogenic hydrogen is stored under supercritical pressure, that is, at least at 13 bar absolute, or at a significantly higher pressure, that is, at 150 bar or more, and/or during filling of the tank, such hydrogen can be filled into a suitable cryo-compressed tank under supercritical pressure.
- supercritical pressure that is, at least at 13 bar absolute, or at a significantly higher pressure, that is, at 150 bar or more, and/or during filling of the tank, such hydrogen can be filled into a suitable cryo-compressed tank under supercritical pressure.
- this minimum pressure level in the tank is set by way of a targeted introduction of heat into the cryo tank.
- This heat input is achieved in that after a sub quantity of the hydrogen, removed from the tank, has been heated in an external heat exchanger, it is conveyed as the heat carrying medium through an (internal) heat exchanger, provided in the cryo tank. At the same time heat is dissipated to the hydrogen stored in the cryo tank. After flowing through this internal heat exchanger, the heat carrying hydrogen is returned again to the supply line leading to the consumer.
- cryogenic hydrogen can be stored at absolute pressure values in a magnitude of 13 bar or more—that is, up to, for example, 350 bar, as mentioned in the above described U.S. Pat. No. 6,708,502 B1, the object is to provide an operating method that is simpler than that described in said prior art.
- the solution to this problem is characterized in that over a period of time that significantly exceeds the cycle times of a conventional frequency valve, either the removed amount of hydrogen, which has been heated, is guided without limitation into the heat exchanger, provided in the cryo-compressed tank, the tank pressure regulating valve being completely open, or no return of the heated hydrogen into the heat exchanger, provided in the cryo-compressed tank, occurs at all; and that downstream of the branching off of the branch line, the supply line has a pressure regulating unit, which ensures that irrespective of the changes in the pressure in the supply line caused upstream of this pressure regulating unit by switching the tank pressure regulating valve, a sufficient and continuous supply of hydrogen to the consumer at the pressure required is guaranteed.
- the invention proposes, instead of the known expensive control element of the tank internal pressure for the tank pressure regulating valve, provided to this end, a simple so-called “black and white operating mode” with long cycle times, to the effect that this tank pressure regulating valve, which continues to be actuated as a function of the internal pressure in the cryo-compressed tank, is alternatingly either totally closed or totally open over a relatively long period of time, which significantly exceeds the typical cycle times of a conventional frequency valve.
- the range of the tank pressure threshold values of a control element which actuates the tank pressure regulating valve, that is, opens and/or closes said valve, must be set correspondingly wide. It has been recognized that the pressure fluctuations, which are automatically larger and/or relatively large with such a control strategy and which occur in a supply line conveying the hydrogen taken from the tank, can be tolerated, if downstream of the branching off of the branch line from the supply line, this supply line has a pressure regulating unit, as stated above.
- the tank pressure regulating valve can remain continuously open, especially if chronologically thereafter the pressure value in the cryo-compressed tank rises.
- This pressure value exceeds an upper threshold value, cited in the previous paragraph, for the actuation of the tank pressure regulating valve, in more concise terms, for closing this valve.
- FIG. 1 is a schematic diagram showing, in principle, a cryo-compressed tank including its peripherals;
- FIG. 2 is a diagram of the tank internal pressure with respect to the filling degree of the cryo-compressed tank.
- FIG. 1 shows in principle a cryo-compressed tank, including its peripheral equipment required for understanding the present invention.
- the reference numeral 1 stands for the entire cryo-compressed tank, in which cryogenic hydrogen that serves to supply a consumer (not illustrated), for example, an internal combustion engine and/or a fuel cell of a motor vehicle, can be stored at absolute pressure values of the tank internal pressure in a magnitude of 150 bar or more, but at least under supercritical pressure at 13 bar or more.
- This cryo-compressed tank 1 consists of a pressure-proof inner tank 1 a , inside of which is stored the cryogenic hydrogen, and, furthermore, an insulating layer 1 b , which envelops the inner tank 1 a and which in essence has a vacuum, as well as an outer shell 1 c , enclosing this vacuum.
- the inner tank 1 a can be filled with cryogenic hydrogen under supercritical pressure by way of a tank filling line 2 .
- the hydrogen can be taken from the inner tank 1 a by way of a removal line 3 , which empties into a cryo valve unit 4 , which is shown only as a rough outline and is not essential for the present explanation.
- Attached to this valve unit 4 is a first, or rather external, heat exchanger 5 , through which are guided, on the one hand, a first heat carrying circuit 15 and secondly a supply line 6 , which follows the removal line 3 and which ultimately leads to the aforesaid consumer.
- the supply line 6 is connected in a heat carrying manner to the first heat carrying circuit 15 , so that the hydrogen, conveyed in the supply line 6 , is heated in the external heat exchanger 5 .
- the first external heat exchanger 5 follows a second valve unit 7 .
- the supply line 5 is guided through this second valve unit 7 while at the same time passing through a tank pressure regulating valve 7 a and a pressure regulating unit 7 b .
- a so-called branch line 8 branches off of the tank pressure regulating valve 7 a .
- the hydrogen, which was removed from the cryo-compressed tank 1 and heated in the first heat exchanger 5 is fed into a second (internal) heat exchanger 9 , provided inside the inner tank 1 a of the cryo-compressed tank 1 .
- this hydrogen After flowing through this second heat exchanger 9 , which is provided in the cryo-compressed tank 1 , this hydrogen is fed over a return line 10 into the supply line 5 , downstream of the branching off of the branch line 8 .
- this return line 10 is guided beforehand through the first external heat exchanger 5 , in which the hydrogen, which has cooled down in the second internal heat exchanger 9 , is heated again by the heat exchange with the said heat carrying circuit 15 . Therefore, the hydrogen, which was conveyed through the branch line 8 and the second internal heat exchanger 9 and the return line 10 , acts as the heat carrying medium that serves to heat the hydrogen, stored in the cryo-compressed tank 1 .
- this temperature increase is controlled by feeding the heat carrying medium to the internal heat exchanger 9 and by the switching strategy of the tank pressure regulating valve 7 a , said strategy having already been explained in detail above in conjunction with the description of the figure.
- FIG. 2 shows a diagram, in which the profile of the tank internal pressure, plotted on the ordinate, over the filling degree of the cryo-compressed tank 1 from FIG. 1 , more precisely the inner tank 1 a of the same, which is plotted on the abscissa, is shown as the mass of stored hydrogen (“H 2 mass”).
- p tank,min stands for the admitted minimum tank internal pressure (in the inner tank 1 a ); and “p drive,min ” stands for the minimum pressure value, which the hydrogen, removed from the cryo-compressed tank 1 , has to exhibit in order to be usable in the consumer, in this case an internal combustion engine which acts as the vehicle drive unit, without any operational restrictions of the consumer (i.e., the internal combustion engine). Although the removed hydrogen can still be used at lower pressure values, the consumer is then operable only to a limited degree. In particular, the maximum possible power of the internal combustion engine can no longer be achieved.
- m tank,full stands for a 100% filling degree of the cryo-compressed tank 1
- m tank,empty stands for a minimum filling degree, which under marginal operating conditions cannot be physically undershot. That is, since a non-removable residual amount of hydrogen (H 2 ), which is denoted with these words in FIG. 2 , remains in the tank, it is self-evident that the tank cannot be totally emptied.
- the tank When the cryo-compressed tank 1 is totally filled, that is, 100% full, the tank exhibits a high internal pressure that is above the pressure value p drive,min .
- the internal pressure in the inner tank 1 a Naturally decreases, when the tank pressure regulating valve 7 a (and, thus, the internal heat exchanger 9 , through which there is no flow (see FIG. 1 )) is initially closed.
- the tank pressure regulating valve 7 a is moved again into its original switching state, in which there was no hydrogen flow whatsoever from the supply line 5 into the branch line 8 , in order not to allow the internal pressure in the tank to continue to increase.
- the tank pressure regulating valve 7 a in turn is held over a longer period of time, which significantly exceeds the typical cycle times of a conventional frequency valve, until once again the lower tank pressure threshold value, that is, the pressure value p drive,min , is reached.
- the method which is proposed herein in general, that is, without the so-called reserve control, is characterized by its ease of implementation with negligibly few demands on the implementing control unit and technology and/or on the corresponding components.
- the number of switching steps (“open” and/or “closed”), to be executed by the tank pressure regulating valve 7 a is significantly smaller than in the case of a continuous pressure regulation on a substantially constant pressure level, which is practiced in the aforementioned “hydrogen 7” vehicle.
- the switching times of the tank pressure regulating valve 7 a can be, as a function of the amount of hydrogen that is removed from the inner tank, in a magnitude of 15 minutes and more, thus, significantly above the typical cycle times of a conventional frequency valve, whereas the upper and lower threshold value for actuating the tank pressure regulating valve 7 a can differ, for example, by 10 bar and more, that is (p 1 ⁇ p drive,min ⁇ 10 bar).
- this and a plurality of details can be designed so as to deviate from the above embodiment without departing from the content of the patent claims.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Catching Or Destruction (AREA)
Abstract
Description
Claims (4)
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102007057978A DE102007057978A1 (en) | 2007-12-03 | 2007-12-03 | Operating procedure for a cryopressure tank |
| DE102007057978.2 | 2007-12-03 | ||
| DE102007057978 | 2007-12-03 | ||
| PCT/EP2008/009890 WO2009071208A1 (en) | 2007-12-03 | 2008-11-21 | Operating method for a cryopressure tank |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/EP2008/009890 Continuation WO2009071208A1 (en) | 2007-12-03 | 2008-11-21 | Operating method for a cryopressure tank |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20100236259A1 US20100236259A1 (en) | 2010-09-23 |
| US9625094B2 true US9625094B2 (en) | 2017-04-18 |
Family
ID=40377445
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/792,331 Expired - Fee Related US9625094B2 (en) | 2007-12-03 | 2010-06-02 | Operating method for a cryo-compressed tank |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9625094B2 (en) |
| EP (1) | EP2217845B1 (en) |
| AT (1) | ATE507432T1 (en) |
| DE (2) | DE102007057978A1 (en) |
| WO (1) | WO2009071208A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10850825B2 (en) | 2017-08-18 | 2020-12-01 | Arianegroup Gmbh | Cooling of a vaporized content of a liquefied gas for the purpose of powering machinery, plants or vehicles |
| US20240240762A1 (en) * | 2023-01-13 | 2024-07-18 | Magna Energy Storage Systems Gesmbh | Cryogenic tank comprising a withdrawal device |
Families Citing this family (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102012204818A1 (en) | 2012-03-26 | 2013-09-26 | Bayerische Motoren Werke Aktiengesellschaft | Operating procedure for a cryogenic pressure tank |
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| US10850825B2 (en) | 2017-08-18 | 2020-12-01 | Arianegroup Gmbh | Cooling of a vaporized content of a liquefied gas for the purpose of powering machinery, plants or vehicles |
| US20240240762A1 (en) * | 2023-01-13 | 2024-07-18 | Magna Energy Storage Systems Gesmbh | Cryogenic tank comprising a withdrawal device |
Also Published As
| Publication number | Publication date |
|---|---|
| DE502008003383D1 (en) | 2011-06-09 |
| EP2217845B1 (en) | 2011-04-27 |
| DE102007057978A1 (en) | 2009-06-04 |
| ATE507432T1 (en) | 2011-05-15 |
| EP2217845A1 (en) | 2010-08-18 |
| US20100236259A1 (en) | 2010-09-23 |
| WO2009071208A1 (en) | 2009-06-11 |
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